FR2955154B1 - THRUST INVERTER FOR TURBO AIRCRAFT WITH DOUBLE FLOW SEMI-BURIAL - Google Patents

THRUST INVERTER FOR TURBO AIRCRAFT WITH DOUBLE FLOW SEMI-BURIAL

Info

Publication number
FR2955154B1
FR2955154B1 FR1050093A FR1050093A FR2955154B1 FR 2955154 B1 FR2955154 B1 FR 2955154B1 FR 1050093 A FR1050093 A FR 1050093A FR 1050093 A FR1050093 A FR 1050093A FR 2955154 B1 FR2955154 B1 FR 2955154B1
Authority
FR
France
Prior art keywords
burial
double flow
thrust inverter
flow semi
turbo
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR1050093A
Other languages
French (fr)
Other versions
FR2955154A1 (en
Inventor
Jacques Herve Marche
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1050093A priority Critical patent/FR2955154B1/en
Priority to US13/520,917 priority patent/US9062626B2/en
Priority to PCT/FR2010/052918 priority patent/WO2011083256A1/en
Publication of FR2955154A1 publication Critical patent/FR2955154A1/en
Application granted granted Critical
Publication of FR2955154B1 publication Critical patent/FR2955154B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/90—Braking
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
FR1050093A 2010-01-08 2010-01-08 THRUST INVERTER FOR TURBO AIRCRAFT WITH DOUBLE FLOW SEMI-BURIAL Expired - Fee Related FR2955154B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1050093A FR2955154B1 (en) 2010-01-08 2010-01-08 THRUST INVERTER FOR TURBO AIRCRAFT WITH DOUBLE FLOW SEMI-BURIAL
US13/520,917 US9062626B2 (en) 2010-01-08 2010-12-27 Thrust reverser for an aircraft having semi-recessed turbofan engines
PCT/FR2010/052918 WO2011083256A1 (en) 2010-01-08 2010-12-27 Thrust reverser for an aircraft having semi-recessed turbofan engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1050093A FR2955154B1 (en) 2010-01-08 2010-01-08 THRUST INVERTER FOR TURBO AIRCRAFT WITH DOUBLE FLOW SEMI-BURIAL

Publications (2)

Publication Number Publication Date
FR2955154A1 FR2955154A1 (en) 2011-07-15
FR2955154B1 true FR2955154B1 (en) 2012-01-06

Family

ID=42350361

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1050093A Expired - Fee Related FR2955154B1 (en) 2010-01-08 2010-01-08 THRUST INVERTER FOR TURBO AIRCRAFT WITH DOUBLE FLOW SEMI-BURIAL

Country Status (3)

Country Link
US (1) US9062626B2 (en)
FR (1) FR2955154B1 (en)
WO (1) WO2011083256A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014197056A2 (en) * 2013-03-14 2014-12-11 United Technologies Corporation Twin target thrust reverser module
PL235797B1 (en) 2018-02-21 2020-10-19 Gen Electric Bell-shaped nozzle unit for gas-turbine engines
US11286879B2 (en) * 2018-07-02 2022-03-29 Rohr, Inc. Target door reverser wit h non-parallel hinge lines
GB2599686A (en) 2020-10-09 2022-04-13 Rolls Royce Plc An improved turbofan gas turbine engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3658279A (en) * 1970-04-21 1972-04-25 Lockheed Aircraft Corp Integrated propulsion system
US4030687A (en) * 1976-02-23 1977-06-21 The Boeing Company Articulated nozzle for upper surface blown aircraft
GB1534583A (en) * 1976-06-08 1978-12-06 Short Bros Ltd Reversal of thrust in gas turbine engines
FR2698913B1 (en) 1992-12-04 1995-02-03 Hurel Dubois Avions Door thrust reverser assembly equipped with a jet control device.
FR2741114B1 (en) 1995-11-15 1997-12-05 Hispano Suiza Sa DOWNSTREAM TURBOREACTOR DRIVE INVERTER TENDING TO BALANCING
FR2757901B1 (en) * 1996-12-26 1999-01-29 Hispano Suiza Sa DOWNSTREAM DOUBLE FLOW TURBOREACTOR DRIVE INVERTER
FR2812035B1 (en) 2000-07-24 2003-08-29 Hurel Dubois Avions IMPROVEMENTS ON DRIVE INVERTERS FOR JET ENGINES OF THE GRID TYPE
FR2914956A1 (en) 2007-04-12 2008-10-17 Aircelle Sa NACELLE FOR TURBOJET ENGINEER EQUIPPED WITH A FORWARD REVERSAL SYSTEM

Also Published As

Publication number Publication date
US9062626B2 (en) 2015-06-23
FR2955154A1 (en) 2011-07-15
US20130097998A1 (en) 2013-04-25
WO2011083256A1 (en) 2011-07-14

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